It is an ultra-light, single-seat, conventional helicopter, powered by a Rotax engine. Its development emerged from the need for an aircraft capable of being used for evaluating different solutions in flight, as well as systems to be used in the CH-5. This turned out to be an aircraft with excellent maneuvering and stability. The main frame is made of steel tubes and the blades are made of composite materials. The command system is unique and patented by Augusto Cicaré. The first flight was achieved in 1987.
Design authority: Cicaré S.A.
Primary manufacturer: Cicaré S.A.
Parent type: No type defined
Aircraft status: Operational
VTOL type: Helicopter
Lift devices: 1 Single main rotor
Dedicated control device: 1 Tail rotor
Crew required: 1 in Other arrangement
Landing gear: Skids